CN107937831B - Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process - Google Patents

Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process Download PDF

Info

Publication number
CN107937831B
CN107937831B CN201711140686.4A CN201711140686A CN107937831B CN 107937831 B CN107937831 B CN 107937831B CN 201711140686 A CN201711140686 A CN 201711140686A CN 107937831 B CN107937831 B CN 107937831B
Authority
CN
China
Prior art keywords
forging
temperature
blank
steel alloy
12cr2mo1v
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201711140686.4A
Other languages
Chinese (zh)
Other versions
CN107937831A (en
Inventor
祁庆花
赵子文
王亚安
温铁军
王晓莉
张潇潇
李七平
秦卓
韩文科
杨德生
曹琨
张静
王炜
高超
刘林
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lanzhou Ls Energy Equipment Engineering Research Institute Co ltd
Lanzhou LS Group Co Ltd
Original Assignee
Lanzhou Ls Energy Equipment Engineering Research Institute Co ltd
Lanzhou LS Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lanzhou Ls Energy Equipment Engineering Research Institute Co ltd, Lanzhou LS Group Co Ltd filed Critical Lanzhou Ls Energy Equipment Engineering Research Institute Co ltd
Priority to CN201711140686.4A priority Critical patent/CN107937831B/en
Publication of CN107937831A publication Critical patent/CN107937831A/en
Application granted granted Critical
Publication of CN107937831B publication Critical patent/CN107937831B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/005Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Forging (AREA)

Abstract

The invention discloses a kind of pressure vessel 12Cr2Mo1V steel alloy, by weight percentage, Main Components include C, Si, Mn, P, S, Cr, Mo, V, Ti, B, Nb, Ni and Al to the chemical component of the 12Cr2Mo1V steel alloy;Residual elements include As, Sn, Sb, Cu, Ca and portion gas element, and surplus is Fe and inevitable impurity.The forging process of blank is 5 fire in the forging heat treatment process of the steel alloy, forging ratio 8, and the initial heating temperature of blank is scheduled on 1250 DEG C, and the final forging temperature of each process requires to be greater than 900 DEG C, and final forging temperature of last fire is greater than 860 DEG C of %;The steel alloy met the requirements using the heat treatment process of annealing, quenching, tempering.Steel alloy prepared by the present invention room temperature with higher and elevated temperature strength, hardness, good low-temperature impact toughness, anti-temper brittleness and higher creep strength and creep rupture strength.

Description

Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process
Technical field
The present invention relates to the technology field of Steel material, specifically a kind of pressure vessel 12Cr2Mo1V Steel alloy and its forging heat treatment process.
Background technique
In recent years, in terms of petroleum refining industry, coalification chemical container, nuclear pressure container industrial expansion trend, equipment technology with Device gradually develops to enlargement, high parameter direction, undoubtedly proposes more to the process equipment of construction of pressure vessel part High requirement, due to being limited by process equipment (such as plate bending machine) ability, pressure vessel is increasingly prone to adopt with structural member With forge welding structure, meanwhile, the operating condition of the harshness such as high temperature, high pressure of pressure vessel proposes higher want to the selection of material It asks, it is heavy smithwelding that 12Cr2Mo1V steel alloy, which has creep strength more higher than 12Cr2Mo1 steel alloy and creep rupture strength, The ideal material of formula pressure vessel.NB/T47008-2017 standard " bearing device carbon steel and alloy steel forging " is right 12Cr2Mo1V Steel material ingredient and performance have clearly stipulate that still to the 12Cr2Mo1V steel weight of acquisition excellent combination property Formula pressure container forgeable piece is welded in swaged forging, needs to optimize material composition proportion, and reasonably select the smelting, forging and heat of forging Treatment process.
Summary of the invention
The object of the present invention is to provide a kind of pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process, protect Card meets wanting for standard in terms of the comprehensive performances such as intensity, hardness, low-temperature impact toughness, anti-temper brittleness and creep rupture strength It asks.
In order to achieve the above objectives, the technical solution used in the present invention are as follows:
A kind of pressure vessel 12Cr2Mo1V steel alloy, the chemical component of the 12Cr2Mo1V steel alloy is with weight percent It include following component C: 0.14-0.15% than meter;Si:0.04-0.09%;Mn:0.55-0.60%;P :≤0.005%;S :≤ 0.003%;Cr:2.40-2.50%;Mo:0.95-1.05%;V:0.25-0.30%;Ti:0.010-0.030%;B:0.0008- 0.0015%;Nb:0.025-0.040%;Ni:0.15-0.20%;Al:0.015-0.030%;Residual elements As≤0.007%;Sn≤ 0.004%;Sb≤0.003%;Cu≤0.08%;Ca≤0.015%;Elemental gas [H]≤0.00015%;[O]≤0.0020%;[N] ≤0.0070%;Surplus is Fe and inevitable impurity.
The chemical component of a kind of forging heat treatment process of pressure vessel 12Cr2Mo1V steel alloy, the steel alloy meets Above-mentioned requirements prepare the raw material of 12Cr2Mo1V steel alloy using EBT electric arc furnaces-LF furnace refining-VD vacuum refining-die casting process Route carries out the smelting casting of steel ingot, forms cylinder blank, and the forging process of blank is 5 fire, and forging ratio 8 is specific to wrap Include following steps:
Step 1: chamfered edge, is heated to 1250 DEG C of temperature for blank for the first time, keeps the temperature 7 hours, it is ensured that blank burning is even to be grilled thoroughly, It comes out of the stove, thick bar hold, chamfered edge, the outer diameter of chamfered edge to blank is D1 in upper and lower flat pattern anvil;Pressure-sizing jaw again, final forging temperature ≥900℃;
Step 2: jumping-up, will be again heated to 1250 DEG C of temperature by the blank of step 1 processing, keeps the temperature 6 hours, out Furnace, the jumping-up in jumping-up drain cap, blank upsetting to outer diameter is D2 by upper ball adding face upset plate entirety jumping-up, and height dimension is H1, final forging temperature >=900 DEG C;
Step 3: pulling out for the first time, the blank third time by step 2 processing is heated to 1250 DEG C of temperature, heat preservation 6 Hour, it comes out of the stove, using WHF forging method, suppress pulling using the wide anvil that width is 1000mm, drafts 300-200mm, until The cross section size dimension of blank be L1, chamfering, be rounded to blank outer diameter be D3, chop riser end 1. and mouth of a river end 2., The cutting length of blank is having a size of L2, final forging temperature >=900 DEG C;
Step 4: rushing centre bore, blank the 4th time by step 3 processing is heated to 1250 DEG C of temperature, heat preservation 4 is small When, it comes out of the stove, by blank jumping-up to height having a size of H2, outer diameter D4, with the dinking primary drying center of diameter D5=450mm Core material is removed in hole, and the size of saddle support reaming to centre bore is D6, and the outer diameter of blank is D7, final forging temperature >=900 DEG C at this time;
Step 5: second pulls out, by the blank by step 4 processing be 500mm with diameter plug in upper flat, lower V It is pulled out in swage block, first pulls out both ends, then pull out centre, and ensure uniform wall thickness, then upper saddle support reaming, shaping, obtain meeting design The forging that size requires, final forging temperature >=860 DEG C;
The forging forged by above-mentioned steps is heat-treated again, the pressure vessel for obtaining meeting design requirement is used 12Cr2Mo1V steel alloy.
Preferably, the forging heat treatment process the following steps are included:
Annealing: forging to be heated is put into heat-treatment furnace, 400 DEG C of heat preservation 4h, heat-treatment furnace is with the liter of≤60 DEG C/h Warm speed is heated to 710 ± 10 DEG C of heat preservation 8h, then is heated to 930 ± 10 DEG C of heat preservation 8h with the heating rate of≤120 DEG C/h, with≤ The cooling rate furnace cooling of 70 DEG C/h is come out of the stove air-cooled to 400 DEG C;
Quenching: the shove charge at≤400 DEG C by the forging after annealing is heated to 930 ± 10 with the heating rate of≤100 DEG C/h DEG C heat preservation 8h, water cooling of coming out of the stove;
Tempering: the third time shove charge at≤400 DEG C by quenched forging is heated to the heating rate of≤100 DEG C/h 710 ± 10 DEG C of heat preservation 8h, come out of the stove air-cooled, obtain the pressure vessel 12Cr2Mo1V steel alloy for meeting design requirement.
Preferably, forging is to obtain good tissue and comprehensive mechanical property in the quenching Step, it is desirable that forging quenching Water temperature≤25 DEG C before entering water;In hardening step, using the method for quenching is proposed, i.e., the forging for heating fresh baked is entered into water completely and is kept After 2min, leaves the water break forging surface air film rapidly, be repeated 2 times, then forging is entered into water, realize the rapid cooling of forging.
The chemical component of 12Cr2Mo1V steel alloy of the present invention is in NB/T47008-2017 standard " bearing device carbon Plain steel and alloy steel forging " it is optimized on the basis of claimed range, wherein C element content is to guarantee that alloy hardness of steel meets mark The principal element of alignment request, C element content is low, and intensity can not meet requirement;C element content is high, can reduce 12Cr2Mo1V alloy The low-temperature flexibility and weldability of steel, it is contemplated that the steel grade belongs to low-alloy steel, therefore the control of C element content is in standard requirements range The upper limit.Si element is the essential element that ferrite is formed, and be intensifier is also to promote the brittle factor, and Si element oneself will not Cause embrittlement, but play a driving role to the embrittlement of P element: when P element content is high, P element can be usually extruded into crystalline substance by Si member (when heat treatment after forging cooling velocity is slow, times of tempering is more and causes also make embrittlement when the big Mr. Yu's value of tempering parameter Pt value at boundary Factor crystal boundary is precipitated);And O element also can be combined into SiO with Si element2Type oxide is mingled with wherein, and is enriched with to grain boundaries, Cause grain boundaries brittle;Suitable Si constituent content can reduce austenite transformation temperature, to inhibit the analysis of pro-eutectoid ferrite Out, tiny bainite structure is advantageously formed, to improve the intensity and toughness of steel alloy;Mn element, Ni element were due to both The harden ability that steel can be improved can improve the low-temperature flexibility of steel again, therefore Mn element, Ni control of element are in standard requirements range The upper limit.Mo element can improve the harden ability of steel and mitigate steel belt roof bolt brittleness, mark so Mo constituent content should control The upper limit of alignment request range;V element can be improved the harden ability of steel and mechanical behavior under high temperature and can refine crystal grain, and have precipitating Invigoration effect, but excessive V element is easy to produce forge crack, so middle limit of the V element control in standard requirements range.Ti member Element is similar with the effect of V element, and TiC stable carbide is precipitated after heat treatment.Nb element belongs to the microalloy element in steel alloy, Its content of strict control is needed, Nb constituent content is excessively high to make the segregation of steel ingot center portion coarse, there is the carbide of Nb element, thus Cause the toughness of steel alloy to decline, thus control Nb element content be not easy it is excessively high.Pressure vessel of the present invention is used 12Cr2Mo1V steel alloy is extremely stringent to the limitation of the harmful elements such as Cu, As, Sn, Sb, proposes extremely to above-mentioned harmful element Stringent control requirement.Pressure vessel of the present invention has good degree of purity with 12Cr2Mo1V steel alloy, and has good Plasticity, toughness require the harmful elements such as S, P, H, O, N and elemental gas relatively stringent.
Pressure vessel of the present invention is with 12Cr2Mo1V steel alloy using conventional smelting pouring technology.
Beneficial effects of the present invention:
(1) present invention is matched with 12Cr2Mo1V alloy composition and is reasonably selected smelting, forging by optimization pressure container And heat treatment process, so that 12Cr2Mo1V alloy steel forging room temperature with higher and elevated temperature strength, hardness, good low temperature Impact flexibility, anti-temper brittleness and higher creep strength and creep rupture strength are repeatedly produced verifying and measure its intensity, hard Degree meets the requirement of NB/T47008-2017 standard " bearing device carbon steel and alloy steel forging ";
(2) pressure vessel -30 DEG C of low-temperature impact toughness of 12Cr2Mo1V steel alloy of technique of the present invention manufacture are utilized (Kv2) > 300J, temper brittleness sensibility evaluate < -80 DEG C of VTr54 of VTr54+3.0 Δ, and performance indexes all has larger Surplus capacity.
(3) forging of pressure vessel of the present invention 12Cr2Mo1V alloy steel forging, heat treatment process are easy in fact It applies, the alloyed steel ingot of acquisition meets the requirement of design.
Detailed description of the invention
Fig. 1 is the blank structure schematic diagram of forging technology step 1 chamfered edge;
Fig. 2 is the blank structure schematic diagram of forging technology step 2 jumping-up;
Fig. 3, Fig. 4 are the blank structure schematic diagrames of forging technology step 3 pulling for the first time;
Fig. 5, Fig. 6 are the blank structure schematic diagrames that forging technology step 4 rushes centre bore;
Fig. 7 is second of forging structural schematic diagram pulled out of forging technology step 5;
Fig. 8, Fig. 9 are the bainite microscopic structure pictures for preparing the forging of completion.
Specific embodiment
The present invention will be further described in detail with reference to the accompanying drawing.
A kind of pressure vessel 12Cr2Mo1V steel alloy, the chemical component of the 12Cr2Mo1V steel alloy is with weight percent It include following component C: 0.14-0.15% than meter;Si:0.04-0.09%;Mn:0.55-0.60%;P :≤0.005%;S :≤ 0.003%;Cr:2.40-2.50%;Mo:0.95-1.05%;V:0.25-0.30%;Ti:0.010-0.030%;B:0.0008- 0.0015%;Nb:0.025-0.040%;Ni:0.15-0.20%;Al:0.015-0.030%;Residual elements As≤0.007%;Sn≤ 0.004%;Sb≤0.003%;Cu≤0.08%;Ca≤0.015%;Elemental gas [H]≤0.00015%;[O]≤0.0020%;[N] ≤0.0070%;Surplus is Fe and inevitable impurity.
The chemical component of a kind of forging heat treatment process of pressure vessel 12Cr2Mo1V steel alloy, the steel alloy meets Above-mentioned requirements prepare the raw material of 12Cr2Mo1V steel alloy using EBT electric arc furnaces-LF furnace refining-VD vacuum refining-die casting process Route carries out the smelting casting of steel ingot, forms cylinder blank, and the forging process of blank is 5 fire, forging ratio 8, with size To be illustrated for outer diameter D=1335mm, internal diameter d=865mm, long L=1950mm cylinder forgings.20T is used according to forge weight The blank of specification, the initial heating temperature of blank are scheduled on 1250 DEG C, and the final forging temperature of each process requires to be greater than 900 DEG C, most The shaping stage of latter fire allows final forging temperature big to control the grain size and the uniform tissue that is refined of finished product forging In 860 DEG C.Forging technology specifically includes the following steps:
Step 1: chamfered edge keeps the temperature 7 hours, it is ensured that blank as shown in Figure 1, blank is heated to 1250 DEG C of temperature for the first time Burn it is even grill thoroughly, come out of the stove, thick bar hold, chamfered edge, in upper and lower flat pattern anvil chamfered edge to blank outer diameter be D1=1000mm;Again Pressure-sizing jaw, final forging temperature >=900 DEG C;
Step 2: jumping-up, as shown in Fig. 2, by being again heated to 1250 DEG C of temperature by the blank of step 1 processing, heat preservation 6 hours, come out of the stove, the jumping-up in jumping-up drain cap, upper ball adding face upset plate entirety jumping-up, by blank upsetting to outer diameter be D2= 2000mm, height dimension are H1=600mm, final forging temperature >=900 DEG C;
Step 3: pulling out for the first time, as shown in figure 3, the blank third time by step 2 processing is heated to temperature 1250 DEG C, 6 hours are kept the temperature, is come out of the stove, using WHF forging method, as shown in figure 4, being suppressed using the wide anvil that width is 1000mm Pulling, drafts 300-200mm, until the cross section size dimension of blank is L1=1050mm, chamfering, the outer diameter for being rounded to blank Having a size of D3=1100mm, chop riser end 1. and mouth of a river end 2., the cutting length of blank having a size of L2=1950mm, final forging temperature >= 900℃;
Step 4: rushing centre bore, as shown in Figure 5, Figure 6, blank the 4th time by step 3 processing is heated to temperature 1250 DEG C, 4 hours are kept the temperature, is come out of the stove, by blank jumping-up to height having a size of H2 ≈ 1000mm, outer diameter is D4=1700mm, is used The dinking primary drying centre bore of diameter D5=450mm removes core material, and the size of saddle support reaming to centre bore is D6=550mm, at this time base The outer diameter of material is D7=1200mm, final forging temperature >=900 DEG C;
Step 5: second pulls out, by the blank by step 4 processing be 500mm with diameter plug in upper flat, lower V It is pulled out in swage block, first pulls out both ends, then pull out centre, and ensure uniform wall thickness, then upper saddle support reaming, shaping, obtain meeting design The forging that size requires, as shown in fig. 7, final forging temperature >=860 DEG C;
The heat treatment process of the forging the following steps are included:
Annealing: forging to be heated is put into heat-treatment furnace, 400 DEG C of heat preservation 4h, heat-treatment furnace is with the liter of≤60 DEG C/h Warm speed is heated to 710 ± 10 DEG C of heat preservation 8h, then is heated to 930 ± 10 DEG C of heat preservation 8h with the heating rate of≤120 DEG C/h, with≤ The cooling rate furnace cooling of 70 DEG C/h is come out of the stove air-cooled to 400 DEG C;
Quenching: the shove charge at≤400 DEG C by the forging after annealing is heated to 930 ± 10 with the heating rate of≤100 DEG C/h DEG C heat preservation 8h, water cooling of coming out of the stove;Forging is to obtain good tissue and comprehensive mechanical property, it is desirable that the water temperature before forging quenching water-inlet ≤25℃;In hardening step, using the method for quenching is proposed, i.e., after the forging for heating fresh baked being entered water holding 2min completely, mention rapidly The water surface breaks forging surface air film out, is repeated 2 times, then forging is entered water, realizes the rapid cooling of forging.
Tempering: the third time shove charge at≤400 DEG C by quenched forging is heated to the heating rate of≤100 DEG C/h 710 ± 10 DEG C of heat preservation 8h, come out of the stove air-cooled, obtain the pressure vessel 12Cr2Mo1V steel alloy for meeting design requirement.
Two groups of samples are taken to carry out performance detection respectively the forging prepared according to the method described in the present invention, including room temperature is bent Take intensity (Rel) and tensile strength (Rm), 450 DEG C of high-temperature yield strengths (Rel), -30 DEG C of low-temperature impact toughness (Kv2), Ovshinsky Body grain size, A, B, C, D, Ds class non-metallic inclusion, the evaluation of temper brittleness sensibility, stress-rupture tester, testing result is such as Under:
First group of sample: room-temperature yield strength (Rel) is 549MPa and tensile strength (Rm) is 660MPa, 450 DEG C of high temperature Yield strength (Rel) is 480MPa, and hardness 198HB, -30 DEG C of low-temperature impact toughness (Kv2) are 307J, and autstenitic grain size is 9.0 grades, A, B, C, D, Ds class non-metallic inclusion are respectively less than 0.5 grade, temper brittleness sensibility evaluate VTr54+3.0 Δ VTr54= - 87 DEG C, microscopic structure is bainite tempered structure (as shown in Figure 8).
Second group of sample: room-temperature yield strength (Rel) is 542MPa and tensile strength (Rm) is 654MPa, 450 DEG C of high temperature Yield strength (Rel) is 478MPa, and hardness 197HB, -30 DEG C of low-temperature impact toughness (Kv2) are 310J, and autstenitic grain size is 9.0 grades, A, B, C, D, Ds class non-metallic inclusion are respectively less than 0.5 grade, temper brittleness sensibility evaluate VTr54+3.0 Δ VTr54= - 90 DEG C, microscopic structure is bainite tempered structure (as shown in Figure 9).
Stress-rupture tester: sample keeps 1000h unbroken in the case where temperature is 540 DEG C, stress is 210MPa.
The present invention by optimization pressure container with 12Cr2Mo1V alloy composition match and reasonably select smelt, forging and Heat treatment process, so that 12Cr2Mo1V alloy steel forging room temperature with higher and elevated temperature strength, hardness, good low temperature punching Toughness, anti-temper brittleness and higher creep strength and creep rupture strength are hit, verifying measurement its intensity, hardness are repeatedly produced Meet the requirement of NB/T47008-2017 standard " bearing device carbon steel and alloy steel forging ";Utilize technique of the present invention The pressure vessel of manufacture -30 DEG C of low-temperature impact toughness of 12Cr2Mo1V steel alloy (Kv2) > 300J, temper brittleness sensibility are commented Determine < -80 DEG C of VTr54 of VTr54+3.0 Δ, performance indexes all has biggish surplus capacity.

Claims (3)

1. a kind of forging heat treatment process of pressure vessel 12Cr2Mo1V steel alloy, the chemical component of the steel alloy is with weight Percentages include following component C: 0.14-0.15%;Si:0.04-0.09%;Mn:0.55-0.60%;P :≤0.005%;S :≤ 0.003%;Cr:2.40-2.50%;Mo:0.95-1.05%;V:0.25-0.30%;Ti:0.010-0.030%;B:0.0008- 0.0015%;Nb:0.025-0.040%;Ni:0.15-0.20%;Al:0.015-0.030%;Residual elements As≤0.007%;Sn≤ 0.004%;Sb≤0.003%;Cu≤0.08%;Ca≤0.015%;Elemental gas [H]≤0.00015%;[O]≤0.0020%;[N] ≤0.0070%;Surplus is Fe and inevitable impurity, it is characterised in that: the raw material for preparing 12Cr2Mo1V steel alloy uses EBT electric arc furnaces-LF furnace refining-VD vacuum refining-die casting process route carries out the smelting casting of steel ingot, forms cylinder blank, The forging process of blank be 5 fire, forging ratio 8, specifically includes the following steps:
Step 1: chamfered edge, is heated to 1250 DEG C of temperature for blank for the first time, keeps the temperature 7 hours, it is ensured that blank burning is even to be grilled thoroughly, and is come out of the stove, Thick bar hold, chamfered edge, the outer diameter of chamfered edge to blank is D1 in upper and lower flat pattern anvil;Pressure-sizing jaw again, final forging temperature >=900 ℃;
Step 2: jumping-up, will be again heated to 1250 DEG C of temperature by the blank of step 1 processing, keeps the temperature 6 hours, come out of the stove, Blank upsetting to outer diameter is D2, height dimension H1, end by jumping-up in jumping-up drain cap, upper ball adding face upset plate entirety jumping-up Forge temperature >=900 DEG C;
Step 3: pulling out for the first time, the blank third time by step 2 processing is heated to 1250 DEG C of temperature, keeps the temperature 6 hours, It comes out of the stove, using WHF forging method, carries out suppressing pulling, drafts 300-200mm, until blank using the wide anvil that width is 1000mm Cross section size dimension be L1, chamfering, be rounded to blank outer diameter be D3, chop riser end 1. and mouth of a river end 2., blank Cutting length having a size of L2, final forging temperature >=900 DEG C;
Step 4: rushing centre bore, blank the 4th time by step 3 processing is heated to 1250 DEG C of temperature, keeps the temperature 4 hours, out Furnace goes blank jumping-up to height having a size of H2, outer diameter D4 with the dinking primary drying centre bore of diameter D5=450mm Core material, the size of saddle support reaming to centre bore are D6, and the outer diameter of blank is D7, final forging temperature >=900 DEG C at this time;
Step 5: second pulls out, by the blank by step 4 processing be 500mm with diameter plug in upper flat, lower V-type anvil Middle pulling first pulls out both ends, then pulls out centre, and ensures uniform wall thickness, and then upper saddle support reaming, shaping, obtain meeting design size It is required that forging, final forging temperature >=860 DEG C;
The forging forged by above-mentioned steps is heat-treated again, the pressure vessel for obtaining meeting design requirement is used 12Cr2Mo1V steel alloy.
2. the forging heat treatment process of pressure vessel according to claim 1 12Cr2Mo1V steel alloy, feature exist In: the forging heat treatment process the following steps are included:
Annealing: forging to be heated being put into heat-treatment furnace, 400 DEG C of heat preservation 4h, and heat-treatment furnace is with the heating speed of≤60 DEG C/h Degree is heated to 710 ± 10 DEG C of heat preservation 8h, then is heated to 930 ± 10 DEG C of heat preservation 8h with the heating rate of≤120 DEG C/h, with≤70 DEG C/the cooling rate furnace cooling of h come out of the stove to 400 DEG C it is air-cooled;
Quenching: the shove charge at≤400 DEG C by the forging after annealing is heated to 930 ± 10 DEG C of guarantors with the heating rate of≤100 DEG C/h Warm 8h, water cooling of coming out of the stove;
Tempering: the third time shove charge at≤400 DEG C by quenched forging, 710 are heated to the heating rate of≤100 DEG C/h ± 10 DEG C of heat preservation 8h, come out of the stove air-cooled, obtain the pressure vessel 12Cr2Mo1V steel alloy for meeting design requirement.
3. the forging heat treatment process of pressure vessel according to claim 2 12Cr2Mo1V steel alloy, feature exist In: forging is to obtain good tissue and comprehensive mechanical property in the quenching Step, it is desirable that the water temperature before forging quenching water-inlet ≤25℃;In hardening step, using the method for quenching is proposed, i.e., after the forging for heating fresh baked being entered water holding 2min completely, mention rapidly The water surface breaks forging surface air film out, is repeated 2 times, then forging is entered water, realizes the rapid cooling of forging.
CN201711140686.4A 2017-11-16 2017-11-16 Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process Expired - Fee Related CN107937831B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711140686.4A CN107937831B (en) 2017-11-16 2017-11-16 Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711140686.4A CN107937831B (en) 2017-11-16 2017-11-16 Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process

Publications (2)

Publication Number Publication Date
CN107937831A CN107937831A (en) 2018-04-20
CN107937831B true CN107937831B (en) 2019-09-10

Family

ID=61931512

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711140686.4A Expired - Fee Related CN107937831B (en) 2017-11-16 2017-11-16 Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process

Country Status (1)

Country Link
CN (1) CN107937831B (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110895274A (en) * 2018-09-11 2020-03-20 中国石化工程建设有限公司 Method for testing temper brittleness of steel and application thereof
CN109234648A (en) * 2018-09-20 2019-01-18 天长市兴宇铸造有限公司 A kind of high and cold high-strength rail traffic bogie key components and parts and its casting method
CN109811262B (en) * 2019-02-26 2021-03-12 中信重工机械股份有限公司 Manufacturing process of 2.25Cr1Mo0.25V steel heavy wall thickness hydrogenated forging
CN110227907A (en) * 2019-06-03 2019-09-13 嘉兴市恒工精密机械有限公司 A kind of processing method of high accurate speed reducer gland
CN112238326A (en) * 2019-07-16 2021-01-19 嘉善县联诚机械有限公司 Production process of bearing copper casting sleeve
CN110283974A (en) * 2019-07-22 2019-09-27 洛阳中创重型机械有限公司 A kind of heat treatment process of pressure vessel 12Cr2Mo1V steel forgings
CN110387504A (en) * 2019-07-23 2019-10-29 舞阳钢铁有限责任公司 A kind of thickness limit faces hydrogen chrome molybdenum steel plate and its production method
CN111101060A (en) * 2019-12-31 2020-05-05 苏州雷格姆海洋石油设备科技有限公司 Alloy steel, high-temperature high-pressure sulfur-resistant throttle valve and manufacturing method
CN113388776B (en) * 2020-03-13 2023-04-14 兰州兰石集团有限公司铸锻分公司 F22 material for well control device, forging method and heat treatment process thereof
CN111482770A (en) * 2020-04-20 2020-08-04 苏州雷格姆海洋石油设备科技有限公司 Underwater manifold connecting piece manufacturing process and underwater manifold connecting piece
CN111826506A (en) * 2020-06-08 2020-10-27 舞阳钢铁有限责任公司 Method for producing large-thickness 12Cr2Mo1VR steel plate by forging blank
CN112620560A (en) * 2020-12-02 2021-04-09 南京迪威尔高端制造股份有限公司 18CrNiMo7-6 gear forging and manufacturing method and detection method for overcoming subcutaneous defects of forging
CN114959510B (en) * 2021-02-25 2023-05-09 宝山钢铁股份有限公司 Thick steel plate with tempering brittleness resistance for high-temperature equipment and manufacturing method thereof
CN113981176B (en) * 2021-10-26 2023-07-25 舞阳钢铁有限责任公司 Quenching method for improving low-temperature impact toughness of long-time die welding of chromium-molybdenum steel plate
CN114029436B (en) * 2021-11-09 2023-11-21 二重(德阳)重型装备有限公司 Thermal processing technology of high-strength and high-toughness rotor center body
CN114182176B (en) * 2021-12-06 2022-11-29 中航卓越锻造(无锡)有限公司 High-strength high-toughness low-alloy steel ring forging and manufacturing method thereof
CN114318162B (en) * 2021-12-27 2024-06-04 中航卓越锻造(无锡)有限公司 Flange forging for high-impact-performance water turbine and manufacturing method thereof
CN115029623B (en) * 2022-05-07 2023-08-25 兰州兰石集团有限公司铸锻分公司 Smelting and forging heat treatment process method of 12Cr2Mo1 steel for pressure vessel
CN115595506B (en) * 2022-11-01 2024-04-09 伊莱特能源装备股份有限公司 High-quality low-alloy high-strength plate steel forging and preparation method thereof
CN115852266B (en) * 2022-12-12 2023-09-05 湖南华菱湘潭钢铁有限公司 Production method for improving low-temperature impact toughness and high-temperature performance of ultra-thick hydrogen-bonded steel plate
CN116652096A (en) * 2023-05-04 2023-08-29 中国第一重型机械股份公司 Forging method of long cylinder forging and long cylinder forging

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09296248A (en) * 1996-05-02 1997-11-18 Nkk Corp High strength chromium-molybdenum-tungsten steel
CN102277540A (en) * 2010-06-10 2011-12-14 宝山钢铁股份有限公司 igh temperature PWHT softening and production method thereof
CN105102657A (en) * 2013-03-29 2015-11-25 杰富意钢铁株式会社 Steel material and hydrogen container as well as manufacturing methods therefor
CN105102653A (en) * 2013-03-29 2015-11-25 杰富意钢铁株式会社 Steel structure for hydrogen, and method for manufacturing pressure accumulator for hydrogen and line pipe for hydrogen
CN107109594A (en) * 2014-12-26 2017-08-29 株式会社神户制钢所 The excellent steel plate of hydrogen induced cracking resistance and line-pipes steel pipe

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09296248A (en) * 1996-05-02 1997-11-18 Nkk Corp High strength chromium-molybdenum-tungsten steel
CN102277540A (en) * 2010-06-10 2011-12-14 宝山钢铁股份有限公司 igh temperature PWHT softening and production method thereof
CN105102657A (en) * 2013-03-29 2015-11-25 杰富意钢铁株式会社 Steel material and hydrogen container as well as manufacturing methods therefor
CN105102653A (en) * 2013-03-29 2015-11-25 杰富意钢铁株式会社 Steel structure for hydrogen, and method for manufacturing pressure accumulator for hydrogen and line pipe for hydrogen
CN107109594A (en) * 2014-12-26 2017-08-29 株式会社神户制钢所 The excellent steel plate of hydrogen induced cracking resistance and line-pipes steel pipe

Also Published As

Publication number Publication date
CN107937831A (en) 2018-04-20

Similar Documents

Publication Publication Date Title
CN107937831B (en) Pressure vessel 12Cr2Mo1V steel alloy and its forging heat treatment process
WO2015197007A1 (en) Carburized alloy steel, method for preparing same, and use thereof
CN107557667A (en) A kind of large die-casting mould high performance hot-work die steel and its manufacturing process
CN102477518B (en) Steel used for steam turbine blades and manufacturing method thereof
CN102146547B (en) Alloy steel roller and manufacturing process thereof
JP6369547B2 (en) Low alloy oil well steel pipe
CN108251759B (en) The martensitic stain less steel and its manufacturing method of reversed austenite toughening
CN101886228B (en) Low carbon martensite aged stainless steel with high strength high toughness and high decay resistance performances
CN104630597B (en) A kind of iron nickel and chromium high temperature alloy and its manufacture method
CN109280849A (en) A kind of high performance hot-work die steel and its manufacturing process
CN102747305B (en) Geothermal power generation turbine rotor low alloy steel and geothermal power generation turbine rotor low alloy material and manufacture method thereof
EP3222742B1 (en) Rolled steel bar or rolled wire material for cold-forged component
CN101994066A (en) Deformation induced maraging stainless steel and machining process thereof
CN110484812A (en) A kind of high-performance hot stamping die steel and its manufacturing process
CN106893832A (en) A kind of BQ & P Technologies for Heating Processing of carbides-free shellfish/horse Multiphase Steel
CN106756509B (en) A kind of high-temperature alloy structural steel and its Technology for Heating Processing
CN115612929A (en) Petroleum casing pipe for heavy oil thermal production well and preparation method thereof
WO2007123164A1 (en) Piston ring material for internal combustion engine
CN104451421A (en) High-strength high-toughness bimetallic strip saw blade back steel and preparation method thereof
CN108754335B (en) A kind of the welding structure fire-resistant and weather-resistant steel and production method of yield strength &gt;=550MPa
CN102383050A (en) Cr-Ni based high temperature-resistant oxyaustenitic heat-resistant steel bar and preparation method thereof
CN104131227A (en) Low-alloy heat-resisting steel pipe and manufacturing method thereof
JP6750744B2 (en) Connecting rod
JP3918587B2 (en) Spring steel for cold forming
CN105940135A (en) Turbine rotor material for geothermal power generation and method for manufacturing same

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190910

Termination date: 20211116

CF01 Termination of patent right due to non-payment of annual fee